Analysis of chugging in liquid-bipropellant rocket engines using propellants with different vaporization rates /
Leon M. Wenzel and John R. Szuch.

Description

Main Author

Wenzel, Leon M.

Related Names

Szuch, John R.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : 1965.

Subjects

Liquid oxygen.
Liquid propellants.
Rocket engines > Rocket engines / Combustion.
Liquid propellant rockets > Liquid propellant rockets / Combustion.

Physical Description

12 p. : ill. ; 27 cm.

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